|June 9, 2013, 15:15||
blowing & suction control mechanism on airfoil
Join Date: Mar 2013
Posts: 24Rep Power: 4
i am working on a project that is " NUMERICAL STUDY OF BLOWING AND SUCTION CONTROL MECHANISM ON NACA 0012 AIR FOIL" i want to calculate CL and Cd.i use k-epsilon and k-omega method.but these parameter that i get from solving in FLUENT are far from their in journal.
injection angle=90 (Perpendicular to injection face)
is there any one help me to solve it?!
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